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US6432165B1 - Method for injecting gases into a metallurgical tank - Google Patents

Method for injecting gases into a metallurgical tank Download PDF

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Publication number
US6432165B1
US6432165B1 US09/555,546 US55554600A US6432165B1 US 6432165 B1 US6432165 B1 US 6432165B1 US 55554600 A US55554600 A US 55554600A US 6432165 B1 US6432165 B1 US 6432165B1
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US
United States
Prior art keywords
gas flow
central pipe
gas
pipe
lance
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
US09/555,546
Inventor
Rainer Dittrich
Horst-Dieter Schöler
Andreas Ploch
Manfred Zeimes
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ThyssenKrupp Steel Europe AG
SMS Siemag AG
Original Assignee
SMS Demag AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SMS Demag AG filed Critical SMS Demag AG
Assigned to SMS DEMAG AG reassignment SMS DEMAG AG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: DITTRICH, RAINER, ZEIMES, MANFRED, PLOCH, ANDREAS, SCHOLER, HORST-DIETER
Assigned to THYSSEN KRUPP STAHL AG, SMS DEMAG AG reassignment THYSSEN KRUPP STAHL AG RE-RECORD TO ADD AN ASSIGNEE INADVERTENTLY OMITTED FROM THE COVER SHEET OF A PREVIOUS RECORDING AT REEL 011031 FRAME 0584. ASSIGNORS HEREBY CONFIRM THE ASSIGNMENT OF THE ENTIRE INTEREST. Assignors: DITTRICH, RAINER, ZEIMES, MANFRED, PLOCH, ANDREAS, SCHOLER, HORST-DIETER
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Publication of US6432165B1 publication Critical patent/US6432165B1/en
Assigned to LEBANON CHEMICAL CORPORATION reassignment LEBANON CHEMICAL CORPORATION TERMINATION OF PATENT SECURITY AGREEMENT Assignors: HOMESTEAD, CORP., THE
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21C—PROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
    • C21C7/00—Treating molten ferrous alloys, e.g. steel, not covered by groups C21C1/00 - C21C5/00
    • C21C7/10—Handling in a vacuum
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21C—PROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
    • C21C5/00—Manufacture of carbon-steel, e.g. plain mild steel, medium carbon steel or cast steel or stainless steel
    • C21C5/28—Manufacture of steel in the converter
    • C21C5/42—Constructional features of converters
    • C21C5/46—Details or accessories
    • C21C5/4606—Lances or injectors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D3/00—Charging; Discharging; Manipulation of charge
    • F27D3/16—Introducing a fluid jet or current into the charge
    • F27D2003/168—Introducing a fluid jet or current into the charge through a lance
    • F27D2003/169—Construction of the lance, e.g. lances for injecting particles

Definitions

  • the invention relates to a method for blowing combustible, optionally solids-laden gases into the free space above a molten metal located in a metallurgical vessel, in particular molten steel in an RH vessel which is under vacuum, by means of a cooled lance.
  • the invention further relates to a blowing lance for carrying out the method.
  • WO 97/08348 has disclosed a method for refining metals in a vacuum vessel, in which a lance is used having a central pipe which is surrounded by an encasing pipe which is arranged coaxially.
  • the central pipe is in the form of a straight cylinder and extends all the way to the end of the encasing pipe.
  • the encasing pipe itself diverges conically in its end region.
  • WO 96/16190 has disclosed a multifunctional lance which can be used for the vacuum treatment of steel in an RH vessel [vacuum vessel for removing oxygen from steel] and which allows the processes of oxygen blowing with and without solids and the generation of a combustion flame independently of one another.
  • This multifunctional lance has a displaceable central pipe which is in the form of a straight cylinder and is arranged inside an encasing pipe, which has an end which widens conically, coaxially with respect to this encasing pipe.
  • the invention is based on the object of providing a method and a suitable blowing lance which, by simple design means, considerably reduces the noise emissions without lowering the individual introduction rates of the media, in particular in the combustion phase.
  • the first gas flow which is guided through the central pipe, runs in such a way that, on leaving the end of the central pipe, during re-expansion it comes into contact with the. second gas flow which surrounds it and is guided through the encasing pipe.
  • the first gas flow is reflected by the second gas flow and/or the inner wall of the encasing pipe of the lance and, as a result, is bundled outside the lance, downstream thereof.
  • the blowing lance used in this method has a cooled encasing pipe, in which a central pipe is coaxially arranged, the end of which is designed in the form of a Laval nozzle.
  • the first gas flow which is guided through the central pipe at a pressure of 4 to 6 bar, is set in vibration at the end of the central pipe.
  • This gas which has been set in vibration can be securely bundled even at high gas speeds.
  • a chamber which serves as a vibration generator is provided in that part of the central pipe which is in the form of a Laval nozzle.
  • This chamber is of annular design and substantially follows the inner wall of the Laval nozzle, or alternately is of entirely cylindrical design.
  • the central pipe prefferably be moved axially in a defined manner, in order to keep the noise to a minimum level according to the quantities of gas currently being blown.
  • the encasing pipe at its end to converge conically, at an angle ⁇ of 1 to 10°, over an area corresponding to the distance a, in the direction of gas flow.
  • This embodiment helps to bundle together the first gas flow which emerges from the central pipe.
  • FIG. 1 shows the end region of the blowing lance
  • FIG. 2 shows the arrangement of the vacuum treatment installation
  • FIG. 3 shows the central pipe as a vibration generator.
  • FIG. 1 shows a blowing lance 21 with a central pipe 22 which is surrounded by a water-cooled encasing pipe 26 .
  • the central pipe 22 is mounted centrally inside the encasing pipe 26 by means of spacer elements 29 .
  • the end 23 of the central pipe 22 is designed in the form of a Laval nozzle, with the diameter d.
  • the nozzle opening 24 itself has a wall thickness of b>5 mm, ensuring that the end is sufficiently strong.
  • the central pipe 22 is arranged in such a way inside the encasing pipe 26 that the nozzle opening 24 is at a distance a of from 0.5 to 0.8 ⁇ d from the nozzle opening of the encasing pipe 26 .
  • FIG. 2 shows a metallurgical vessel 11 which is filled with molten material S.
  • An RH vessel 12 which is connected to a vacuum installation 13 and into which a blowing lance 21 projects, projects into the molten material S.
  • the blowing lance 21 is connected to various media supplies, specifically to a cooling medium 31 , to an oxygen supply 32 via oxygen lines 33 , to a fuel-gas supply 34 (such as natural gas) via fuel-gas lines 35 , to a solids supply 36 (such as coal dust) via a solids line 37 , and to an inert-gas supply 38 via an inert-gas line 39 .
  • the individual lines 33 , 35 , 37 and 39 can be blocked by means of suitable valves and fittings.
  • FIG. 3 shows the end 23 of the central pipe 22 having the chambers 25 , 28 as vibration generators.
  • the diameter of the end of the central pipe 22 is d and the wall thickness thereof is b.
  • the length of the Laval nozzle is denoted by L L
  • the critical diameter is denoted by d K .
  • the length of the Laval nozzle is denoted by l a .
  • FIG. 3 shows an annular chamber 25 which is in the form of a Laval nozzle and is of the length l L and diameter D L at the end of the chamber 25 , as seen in the direction of flow.
  • the ratio of the diameter D L to the virtual diameter d L of the Laval nozzle is constant.
  • the right-hand side of the figure shows a cylindrical chamber 28 of a length L Z and with a constant diameter D L .
  • This chamber 28 is at a distance l a from the critical diameter d K of the end 23 which is in the form of a Laval nozzle.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Treatment Of Steel In Its Molten State (AREA)

Abstract

A blowing lance for treating molten metals which are situated in vacuum-treatment vessels, in particular steel in RH vessels, having a central pipe and an encasing pipe which is arranged coaxially with respect to the central pipe and can be cooled by a cooling medium. The central pipe and the encasing pipe are connected to supply lines, which in turn can be connected to an oxygen station, a fuel-gas station and an inert-gas station and to a solids-feed device. In this lance, the cooled encasing pipe is arranged at a distance from the central pipe over its entire length. The free annular area (AR) between the two pipes satisfying the following statement
A R=0.8 to 1.2×A Z
where AZ=free cross-sectional area of the central pipe. The end of the central pipe is designed in the form of a Laval nozzle. The nozzle opening of the central pipe is being arranged at a distance (a) inside the encasing tube,
where a=0.5 to 0.8×d
where d=clear diameter of the central pipe.

Description

BACKGROUND OF THE INVENTION
1. Field of the Invention
The invention relates to a method for blowing combustible, optionally solids-laden gases into the free space above a molten metal located in a metallurgical vessel, in particular molten steel in an RH vessel which is under vacuum, by means of a cooled lance. The invention further relates to a blowing lance for carrying out the method.
2. Discussion of Prior Art
WO 97/08348 has disclosed a method for refining metals in a vacuum vessel, in which a lance is used having a central pipe which is surrounded by an encasing pipe which is arranged coaxially. In this case, the central pipe is in the form of a straight cylinder and extends all the way to the end of the encasing pipe. The encasing pipe itself diverges conically in its end region.
Furthermore, WO 96/16190 has disclosed a multifunctional lance which can be used for the vacuum treatment of steel in an RH vessel [vacuum vessel for removing oxygen from steel] and which allows the processes of oxygen blowing with and without solids and the generation of a combustion flame independently of one another. This multifunctional lance has a displaceable central pipe which is in the form of a straight cylinder and is arranged inside an encasing pipe, which has an end which widens conically, coaxially with respect to this encasing pipe.
Particularly during combustion, operating with these known lances causes considerable noise pollution. A further drawback is the relatively complicated design of the lance.
SUMMARY OF THE INVENTION
The invention is based on the object of providing a method and a suitable blowing lance which, by simple design means, considerably reduces the noise emissions without lowering the individual introduction rates of the media, in particular in the combustion phase.
According to the invention, the first gas flow, which is guided through the central pipe, runs in such a way that, on leaving the end of the central pipe, during re-expansion it comes into contact with the. second gas flow which surrounds it and is guided through the encasing pipe. In the process, the first gas flow is reflected by the second gas flow and/or the inner wall of the encasing pipe of the lance and, as a result, is bundled outside the lance, downstream thereof. Surprisingly, it has emerged that this reflection has scarcely any adverse effect on the output rate, yet the subsequent intensive bundling considerably reduces the noise.
The blowing lance used in this method has a cooled encasing pipe, in which a central pipe is coaxially arranged, the end of which is designed in the form of a Laval nozzle. The nozzle opening of the central pipe ends inside the encasing pipe, specifically at a distance of a=0.5 to 0.8×d, where d is the clear diameter of the central pipe.
In one embodiment, the first gas flow, which is guided through the central pipe at a pressure of 4 to 6 bar, is set in vibration at the end of the central pipe. This gas which has been set in vibration can be securely bundled even at high gas speeds. For this purpose, a chamber which serves as a vibration generator is provided in that part of the central pipe which is in the form of a Laval nozzle. This chamber is of annular design and substantially follows the inner wall of the Laval nozzle, or alternately is of entirely cylindrical design.
In an advantageous embodiment, it is proposed for the central pipe to be moved axially in a defined manner, in order to keep the noise to a minimum level according to the quantities of gas currently being blown.
Furthermore, it is proposed for the encasing pipe at its end to converge conically, at an angle α of 1 to 10°, over an area corresponding to the distance a, in the direction of gas flow. This embodiment helps to bundle together the first gas flow which emerges from the central pipe.
BRIEF DESCRIPTION OF THE DRAWINGS
One example of the invention is illustrated in the appended drawing, in which:
FIG. 1 shows the end region of the blowing lance;
FIG. 2 shows the arrangement of the vacuum treatment installation; and
FIG. 3 shows the central pipe as a vibration generator.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
FIG. 1 shows a blowing lance 21 with a central pipe 22 which is surrounded by a water-cooled encasing pipe 26. The central pipe 22 is mounted centrally inside the encasing pipe 26 by means of spacer elements 29.
The end 23 of the central pipe 22 is designed in the form of a Laval nozzle, with the diameter d. The nozzle opening 24 itself has a wall thickness of b>5 mm, ensuring that the end is sufficiently strong.
The central pipe 22 is arranged in such a way inside the encasing pipe 26 that the nozzle opening 24 is at a distance a of from 0.5 to 0.8×d from the nozzle opening of the encasing pipe 26.
In the bottom part of the picture, the inner wall 27 of the encasing pipe 26 is designed in such a manner that the end converges conically at an angle α=1 to 10° over the region corresponding to distance a, in the direction of gas flow.
FIG. 1a shows a section through the blowing lance and illustrates the free annular area AR between the encasing pipe 26 and the central pipe 22, the size of which is AR=0.8 to 1.2×AZ, where AZ is the clear cross-sectional area of the central pipe.
FIG. 2 shows a metallurgical vessel 11 which is filled with molten material S. An RH vessel 12, which is connected to a vacuum installation 13 and into which a blowing lance 21 projects, projects into the molten material S.
The blowing lance 21 is connected to various media supplies, specifically to a cooling medium 31, to an oxygen supply 32 via oxygen lines 33, to a fuel-gas supply 34 (such as natural gas) via fuel-gas lines 35, to a solids supply 36 (such as coal dust) via a solids line 37, and to an inert-gas supply 38 via an inert-gas line 39. The individual lines 33, 35, 37 and 39 can be blocked by means of suitable valves and fittings.
FIG. 3 shows the end 23 of the central pipe 22 having the chambers 25, 28 as vibration generators. In this case, the diameter of the end of the central pipe 22 is d and the wall thickness thereof is b. The length of the Laval nozzle is denoted by LL, and the critical diameter is denoted by dK. Beginning from the critical diameter dK, in the direction of gas flow, the length of the Laval nozzle is denoted by la.
The left-hand side of FIG. 3 shows an annular chamber 25 which is in the form of a Laval nozzle and is of the length lL and diameter DL at the end of the chamber 25, as seen in the direction of flow. Over the length of the annular chamber 25, which is in the form of a Laval nozzle, the ratio of the diameter DL to the virtual diameter dL of the Laval nozzle is constant.
The right-hand side of the figure shows a cylindrical chamber 28 of a length LZ and with a constant diameter DL. This chamber 28 is at a distance la from the critical diameter dK of the end 23 which is in the form of a Laval nozzle.
If fossil fuel gas is guided through the central pipe and oxygen through the annular chamber or, oxygen through the central pipe and fossil fuel gas through the annular chamber, the oxygen and fuel gas are set in approximately stoichiometric ratios and the pressure pB of the fuel gas and po of the oxygen are set pB/p0=1.4 to 1.8/1.
When oxygen is guided through the central pipe and an inert gas is guided through the annular chamber, given an amount of blown oxygen of m0=3,000 to 4,000 m3/h (s.t.p.), quantitative ratios of the quantity of oxygen m0 and the quantity of inert gas mG are set so that mo/mG=20/1 to 50/1.
The invention is not limited by the embodiments described above which are presented as examples only but can be modified in various ways within the scope of protection defined by the appended patent claims.

Claims (7)

What is claimed is:
1. Method for blowing combustible gases into a free space above a molten metal located in a metallurgical vessel which is under vacuum, by means of a cooled lance, comprising the steps of:
b) adding solid particles to the gas according to a desired procedure;
c) guiding a second gas flow out to beyond the end of the central pipe via an annular chamber arranged coaxially with respect to the central pipe so that the second gas flow surrounds the first gas flow;
d) on leaving the end of the central pipe which is in the form of a Laval nozzle, the first gas flow re-expands and comes into contact with the surrounding second gas flow, is deflected by at least one of the second gas flow and an inner wall of an encasing pipe of the lance, which encasing pipe converges conically in the direction of gas flow, whereby the first gas flow is bundled outside the lance, downstream thereof, the first gas flow guided through the central pipe being a fossil-fuel gas and the second gas flow guided through the annular chamber being oxygen, the process including setting the fuel gas and the oxygen in approximately stoichiometric ratios and setting dynamic pressures pB/poat 1.4 to 1.8/1
where
pB=pressure of the fuel gas, and
po=pressure of the oxygen.
2. A method according to claim 1, wherein the first gas flow is natural gas.
3. A method according to claim 1, including adding solids to the fuel gas.
4. A method according to claim 3, wherein the step of adding solids to the fuel gas includes adding coal dust to the fuel gas.
5. A method according to claim 1, further including setting the first gas flow, which is guided through the central pipe at a pressure (p) where p=4 to 6 bar, in vibration at the end of the central pipe.
6. Method for blowing combustible gases into a free space above a molten metal located in a metallurgical vessel which is under vacuum, by means of a cooled lance, comprising the steps of
a) guiding a first gas flow through a central pipe having an end designed in the form of a Laval nozzle;
b) adding solid particles to the gas according to a desired procedure;
c) guiding a second gas flow out to beyond the end of the central pipe via an annular chamber arranged coaxially with respect to the central pipe so that the second gas flow surrounds the first gas flow;
d) on leaving the end of the central pipe which is in the form of a Laval nozzle, the first gas flow re-expands and comes into contact with the surrounding second gas flow, is deflected by at least one of the second gas flow and an inner wall of an encasing pipe of the lance, which encasing pipe converges conically in the direction of gas flow, whereby the first gas flow is bundled outside the lance, downstream thereof, the first gas flow, which is guided through the central pipe, being oxygen and the second gas flow, which is guided through the annular chamber, being a fossil-fuel gas, the process including setting the oxygen and the fuel gas in approximately stoichiometric ratios and setting pressures pB/po at 1.4 to 1.8/1,
where
pB=pressure of the fuel gas, and
po=pressure of the oxygen.
7. Method for blowing combustible gases into a free space above a molten metal located in a metallurgical vessel which is under vacuum, by means of a cooled lance, comprising the steps of
a) guiding a first gas flow through a central pipe having an end designed in the form of a Laval nozzle;
b) adding solid particles to the gas according to a desired procedure;
c) guiding a second gas flow out to beyond the end of the central pipe via an annular chamber arranged coaxially with respect to the central pipe so that the second gas flow surrounds the first gas flow;
d) on leaving the end of the central pipe which is in the form of a Laval nozzle, the first gas flow re-expands and comes into contact with the surrounding second gas flow, is deflected by at least one of the second gas flow and an inner wall of an encasing pipe of the lance, which encasing pipe converges conically in the direction of gas flow, whereby the first gas flow is bundled outside the lance, downstream thereof, the first gas flow, which is guided through the central pipe, being oxygen, and the second gas flow guided through the annular chamber being inert gas, given an amount of blown oxygen of m0=3,000 to 4,000 m3/h (s.t.p.), quantative ratios m0/mG are set to 20/1 to 50/1
where
m0=quantity of oxygen, and
mG=quantity of insert gas.
US09/555,546 1997-12-04 1998-11-24 Method for injecting gases into a metallurgical tank Expired - Fee Related US6432165B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19755876 1997-12-04
DE19755876A DE19755876C2 (en) 1997-12-04 1997-12-04 Blow lance for treating metallic melts and method for blowing in gases
PCT/DE1998/003512 WO1999029915A1 (en) 1997-12-04 1998-11-24 Method and oxygen lance for injecting gases into a metallurgical tank

Publications (1)

Publication Number Publication Date
US6432165B1 true US6432165B1 (en) 2002-08-13

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US (1) US6432165B1 (en)
EP (1) EP1036205B1 (en)
JP (1) JP2001526320A (en)
KR (1) KR20010032731A (en)
CN (1) CN1280630A (en)
AT (1) ATE224958T1 (en)
AU (1) AU748298B2 (en)
BR (1) BR9814253A (en)
CA (1) CA2312775A1 (en)
DE (2) DE19755876C2 (en)
ES (1) ES2180224T3 (en)
WO (1) WO1999029915A1 (en)

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US20050230885A1 (en) * 2002-04-24 2005-10-20 Cameron Andrew M Lance for injecting particulate material into liquid metal
WO2006105578A1 (en) * 2004-10-18 2006-10-12 Technological Resources Pty Limited Apparatus for injecting solid particulate material into a vessel
US20070012139A1 (en) * 2005-07-13 2007-01-18 Mahoney William J Method for operating a vacuum vessel with a coherent jet
US20110127702A1 (en) * 2009-11-30 2011-06-02 Gautam Vivek Dynamic control of lance utilizing counterflow fluidic techniques
US20110127701A1 (en) * 2009-11-30 2011-06-02 Grant Michael G K Dynamic control of lance utilizing co-flow fluidic techniques
US20110127703A1 (en) * 2009-11-30 2011-06-02 Gautam Vivek Dynamic lances utilizing fluidic techniques
WO2012159179A1 (en) 2011-05-20 2012-11-29 Magnesita Refratários S/A Cooled lance for injecting into a metallurgical vessel
WO2016131118A1 (en) * 2015-02-19 2016-08-25 Lumar Metals Ltda Blow lance assembly for metal manufacturing and refining
US11473776B2 (en) 2017-03-31 2022-10-18 Taiyo Nippon Sanso Corporation Burner, method for operating burner, and method for melting and refining cold iron source

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IT1302798B1 (en) 1998-11-10 2000-09-29 Danieli & C Ohg Sp INTEGRATED DEVICE FOR THE INJECTION OF OXYGEN AND GASTECNOLOGICS AND FOR THE INSUFFLATION OF SOLID MATERIAL IN
ITMI20012278A1 (en) * 2001-10-30 2003-04-30 Techint Spa DEVICE AND METHOD FOR DISCRETE AND CONTINUOUS MEASUREMENT OF THE TEMPERATURE OF LIQUID METAL IN AN OVEN OR CONTAINER FOR ITS PRODUCTION
DE10253463A1 (en) * 2002-11-16 2004-06-03 Gecon Engineering Gmbh Method and device for cooling blowing lances
US20060040048A1 (en) * 2004-08-23 2006-02-23 Taeyoung Han Continuous in-line manufacturing process for high speed coating deposition via a kinetic spray process
ITMI20050241A1 (en) * 2005-02-18 2006-08-19 Techint Spa MULTIFUNCTIONAL INJECTOR AND ITS COMBUSTION PROCEDURE FOR METALLURGICAL TREATMENT IN AN ELECTRIC ARC FURNACE
JP4742855B2 (en) * 2005-12-22 2011-08-10 住友金属工業株式会社 Molten metal refining lance
DE102009022208B4 (en) * 2009-05-20 2013-03-28 Messer Group Gmbh Process for treating molten metals
WO2011024814A1 (en) * 2009-08-28 2011-03-03 株式会社Istc Gas jet device
KR101248940B1 (en) 2011-09-19 2013-04-01 한국수력원자력 주식회사 Crucible of a oxygen suppling apparatus
JP6926928B2 (en) * 2017-10-18 2021-08-25 日本製鉄株式会社 Refining method of molten steel
CN111424137A (en) * 2020-04-13 2020-07-17 攀钢集团攀枝花钢钒有限公司 Gun position control method and system for MFB gun

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US20050230885A1 (en) * 2002-04-24 2005-10-20 Cameron Andrew M Lance for injecting particulate material into liquid metal
US7396503B2 (en) * 2002-04-24 2008-07-08 The Boc Group Plc Lance for injecting particulate material into liquid metal
WO2006105578A1 (en) * 2004-10-18 2006-10-12 Technological Resources Pty Limited Apparatus for injecting solid particulate material into a vessel
US20070012139A1 (en) * 2005-07-13 2007-01-18 Mahoney William J Method for operating a vacuum vessel with a coherent jet
US7297180B2 (en) 2005-07-13 2007-11-20 Praxair Technology, Inc. Method for operating a vacuum vessel with a coherent jet
US20110127701A1 (en) * 2009-11-30 2011-06-02 Grant Michael G K Dynamic control of lance utilizing co-flow fluidic techniques
US20110127702A1 (en) * 2009-11-30 2011-06-02 Gautam Vivek Dynamic control of lance utilizing counterflow fluidic techniques
US20110127703A1 (en) * 2009-11-30 2011-06-02 Gautam Vivek Dynamic lances utilizing fluidic techniques
US8323558B2 (en) * 2009-11-30 2012-12-04 L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Dynamic control of lance utilizing counterflow fluidic techniques
US8377372B2 (en) 2009-11-30 2013-02-19 L'air Liquide Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Dynamic lances utilizing fluidic techniques
WO2012159179A1 (en) 2011-05-20 2012-11-29 Magnesita Refratários S/A Cooled lance for injecting into a metallurgical vessel
WO2016131118A1 (en) * 2015-02-19 2016-08-25 Lumar Metals Ltda Blow lance assembly for metal manufacturing and refining
US11473776B2 (en) 2017-03-31 2022-10-18 Taiyo Nippon Sanso Corporation Burner, method for operating burner, and method for melting and refining cold iron source

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DE59805743D1 (en) 2002-10-31
EP1036205B1 (en) 2002-09-25
EP1036205A1 (en) 2000-09-20
CN1280630A (en) 2001-01-17
AU748298B2 (en) 2002-05-30
AU1869199A (en) 1999-06-28
WO1999029915A1 (en) 1999-06-17
ES2180224T3 (en) 2003-02-01
CA2312775A1 (en) 1999-06-17
JP2001526320A (en) 2001-12-18
DE19755876C2 (en) 2000-02-24
DE19755876A1 (en) 1999-06-17
ATE224958T1 (en) 2002-10-15
BR9814253A (en) 2000-10-03
KR20010032731A (en) 2001-04-25

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